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1. 发明授权

US4253301A Fuel injection staged sectoral combustor for burning low-BTU fuel gas 失效
标题翻译：用于燃烧低BTU燃料气体的燃料喷射分级部门燃烧器
公开(公告)号：US4253301A
公开(公告)日：1981-03-03
申请号：US951181
申请日：1978-10-13
申请人： Robert L. Vogt
发明人： Robert L. Vogt
IPC分类号： F02C7/22 , F23C99/00 , F23R3/00 , F23R3/08 , F23R3/34 , F23R3/36 , F02C3/20
CPC分类号： F23R3/002 , F23R3/34 , F23R3/36 , F23R2900/00002 , F23R2900/00005
摘要： A high-temperature combustor for burning low-BTU coal gas in a gas turbine is described. The combustor comprises a plurality of individual combustor chambers. Each combustor chamber has a main burning zone and a pilot burning zone. A pipe for the low-BTU coal gas is connected to the upstream end of the pilot burning zone; this pipe surrounds a liquid fuel source and is in turn surrounded by an air supply pipe; swirling means are provided between the liquid fuel source and the coal gas pipe and between the gas pipe and the air pipe. Additional preheated air is provided by counter-current coolant air in passages formed by a double wall arrangement of the walls of the main burning zone communicating with passages of a double wall arrangement of the pilot burning zone; this preheated air is turned at the upstream end of the pilot burning zone through swirlers to mix with the original gas and air input (and the liquid fuel input when used) to provide more efficient combustion. One or more fuel injection stages (second stages) are provided for direct input of coal gas into the main burning zone. The countercurrent air coolant passages are connected to swirlers surrounding the input from each second stage to provide additional oxidant.
摘要翻译：描述了用于在燃气轮机中燃烧低BTU煤气的高温燃烧器。燃烧器包括多个单独的燃烧室。每个燃烧室具有主燃烧区和先导燃烧区。用于低BTU煤气的管道连接到先导燃烧区域的上游端; 该管围绕液体燃料源，并由供气管围绕; 在液体燃料源和煤气管之间以及气体管道和空气管之间设置有旋转装置。通过主燃烧区域的壁的双壁布置形成的通道中的逆流冷却剂空气提供额外的预热空气，与主燃烧区的双壁布置的通道连通; 该预热空气通过旋流器在先导燃烧区域的上游端转动，以与原始气体和空气输入（以及使用时的液体燃料输入）混合，以提供更有效的燃烧。提供一个或多个燃料喷射级（第二级），用于将煤气直接输入主燃烧区。逆流空气冷却剂通道连接到围绕来自每个第二级的输入的旋流器以提供附加的氧化剂。

2. 发明申请

US20080209435A1 Scalable workflow management system 审中-公开
标题翻译：可扩展的工作流管理系统
公开(公告)号：US20080209435A1
公开(公告)日：2008-08-28
申请号：US11710154
申请日：2007-02-23
申请人： George R. Dong , Jeffrey A. Wang , Lan Chen , Jin Wang , Anton P. Pavlovich Amirov , Sanjay Jacob , Zhenyu Tang , Patrick J. Baumgartner , Xiaohong Yang , Rou-Peng Huang , Robert L. Vogt
发明人： George R. Dong , Jeffrey A. Wang , Lan Chen , Jin Wang , Anton P. Pavlovich Amirov , Sanjay Jacob , Zhenyu Tang , Patrick J. Baumgartner , Xiaohong Yang , Rou-Peng Huang , Robert L. Vogt
IPC分类号： G06F9/45
CPC分类号： G06Q10/06
摘要： A scalable workflow management system is provided that includes queues for storing work items to be processed. Work items may be placed into the queues by front-end services executing within the workflow management system. When a work item is placed on a queue, it remains on the queue until an appropriate back-end service is available to de-queue the work item, validate the de-queued work item, and process the de-queued work item. Separate queues are provided for storing normal work items, work items generated according to a time schedule, and work items generated by job launching services. The state of operation of the workflow management system may be controlled by an administrative console application.
摘要翻译：提供了可扩展的工作流管理系统，其包括用于存储要处理的工作项的队列。工作项可以通过在工作流管理系统内执行的前端服务放入队列中。当工作项置于队列中时，它将保留在队列上，直到有适当的后端服务可用于对工作项进行排队，验证排队后的工作项，并处理排队后的工作项。提供单独的队列用于存储正常工作项目，根据时间表生成的工作项目以及由作业启动服务生成的工作项目。工作流管理系统的操作状态可以由管理控制台应用来控制。

3. 发明授权

US4916906A Breach-cooled structure 失效
标题翻译：破裂冷却结构
公开(公告)号：US4916906A
公开(公告)日：1990-04-17
申请号：US176482
申请日：1988-03-25
申请人： Robert L. Vogt
发明人： Robert L. Vogt
IPC分类号： F02C7/18 , F01D5/18 , F23R3/00 , F23R3/42
CPC分类号： F23R3/002 , F01D5/188 , F05D2260/201 , F23R2900/03044 , Y02T50/676
摘要： The present invention comprises a method and apparatus for improving cooling of a wall in a gas turbine engine. The method and apparatus provide breach cooling of an imperforate wall, such as a combustor liner, for improving the cooling thereof. The breach cooling includes structure for channeling a cooling fluid as a jet toward an outer surface of the imperforate wall, with the jet having sufficient memontum to breach a boundary layer of the cooling fluid which forms over the wall outer surface to allow the jet to contact the wall outer surface for more effective cooling thereof. In an exemplary embodiment of the invention, the breach-cooled wall is an upstream portion of the gas turbine engine combustor, and the inner surface of the combustor liner facing the combustion gases is characterized by not having a film-cooling boundary layer of air to reduce quenching of the combustion gases for reducing exhaust emissions.
摘要翻译：本发明包括一种用于改善燃气涡轮发动机中的壁的冷却的方法和装置。该方法和装置提供诸如燃烧器衬套的无孔壁的破裂冷却，以改善其冷却。泄漏冷却包括用于将冷却流体作为射流引导到无孔壁的外表面的结构，其中射流具有足够的密度以破坏在壁外表面上形成的冷却流体的边界层，以允许射流接触壁外表面更有效地冷却。在本发明的示例性实施例中，泄漏冷却壁是燃气涡轮发动机燃烧器的上游部分，并且面向燃烧气体的燃烧器衬套的内表面的特征在于不具有膜冷却边界层的空气减少燃烧气体的淬火以减少废气排放。

4. 发明授权

US08359658B2 Secure authoring and execution of user-entered database programming 有权
标题翻译：安全地创建和执行用户输入的数据库编程
公开(公告)号：US08359658B2
公开(公告)日：2013-01-22
申请号：US12049312
申请日：2008-03-15
申请人： Sanjay Jacob , Robert L. Vogt , Kevin Robert Schmidt , Xiaohong Mark Yang , Peiyuan Yan
发明人： Sanjay Jacob , Robert L. Vogt , Kevin Robert Schmidt , Xiaohong Mark Yang , Peiyuan Yan
IPC分类号： G06F21/00
CPC分类号： G06F21/6218 , G06F2221/2145 , G06F2221/2147
摘要： A secure framework for authoring and execution of user-entered database scripts, rules, procedures and other forms of programming is provided. A performance management application is used as an interface between a client data modeling, manipulation or analysis application and one or more data sources or analysis services to prevent malicious or inadvertent implementation of harmful, damaging and/or unauthorized new or modified scripts, rules, procedures or other forms of programming to one or more data sources or data analysis/manipulation services that may be used for retrieving, storing, modifying or using data contained in or affected by the one or more data sources or data analysis/manipulation services.
摘要翻译：提供了用于编辑和执行用户输入的数据库脚本，规则，过程和其他形式的编程的安全框架。性能管理应用程序用作客户端数据建模，操纵或分析应用程序与一个或多个数据源或分析服务之间的接口，以防止恶意或无意中实施有害的，有害的和/或未经授权的新的或修改的脚本，规则，程序或其他形式的编程到可以用于检索，存储，修改或使用由一个或多个数据源或数据分析/操纵服务所包含或受其影响的数据的一个或多个数据源或数据分析/处理服务。

5. 发明申请

US20090133132A1 Secure Authoring and Execution of User-Entered Database Programming 有权
标题翻译：安全的创作和执行用户输入的数据库编程
公开(公告)号：US20090133132A1
公开(公告)日：2009-05-21
申请号：US12049312
申请日：2008-03-15
申请人： Sanjay Jacob , Robert L. Vogt , Kevin Robert Schmidt , Xiaohong Mark Yang , Peiyuan Yan
发明人： Sanjay Jacob , Robert L. Vogt , Kevin Robert Schmidt , Xiaohong Mark Yang , Peiyuan Yan
IPC分类号： G06F21/22
CPC分类号： G06F21/6218 , G06F2221/2145 , G06F2221/2147
摘要： A secure framework for authoring and execution of user-entered database scripts, rules, procedures and other forms of programming is provided. A performance management application is used as an interface between a client data modeling, manipulation or analysis application and one or more data sources or analysis services to prevent malicious or inadvertent implementation of harmful, damaging and/or unauthorized new or modified scripts, rules, procedures or other forms of programming to one or more data sources or data analysis/manipulation services that may be used for retrieving, storing, modifying or using data contained in or affected by the one or more data sources or data analysis/manipulation services.
摘要翻译：提供了用于编辑和执行用户输入的数据库脚本，规则，过程和其他形式的编程的安全框架。性能管理应用程序用作客户端数据建模，操纵或分析应用程序与一个或多个数据源或分析服务之间的接口，以防止恶意或无意中实施有害的，有害的和/或未经授权的新的或修改的脚本，规则，程序或其他形式的编程到可以用于检索，存储，修改或使用由一个或多个数据源或数据分析/操纵服务所包含或受其影响的数据的一个或多个数据源或数据分析/处理服务。

6. 发明授权

US4498288A Fuel injection staged sectoral combustor for burning low-BTU fuel gas 失效
标题翻译：用于燃烧低BTU燃料气体的燃料喷射分级部门燃烧器
公开(公告)号：US4498288A
公开(公告)日：1985-02-12
申请号：US465295
申请日：1983-02-09
申请人： Robert L. Vogt
发明人： Robert L. Vogt
IPC分类号： F23R3/00 , F23R3/34 , F23R3/36 , F02C3/14
CPC分类号： F23R3/36 , F23R3/002 , F23R3/34 , F23R2900/00002 , F23R2900/00005
摘要： A high-temperature combustor for burning low-BTU coal gas in a gas turbine is described. The combustor comprises a plurality of individual combustor chambers. Each combustor chamber has a main burning zone and a pilot burning zone. A pipe for the low-BTU coal gas is connected to the upstream end of the pilot burning zone: this pipe surrounds a liquid fuel source and is in turn surrounded by an air supply pipe: swirling means are provided between the liquid fuel source and the coal gas pipe and between the gas pipe and the air pipe. Additional preheated air is provided by counter-current coolant air in passages formed by a double wall arrangement of the walls of the main burning zone communicating with passages of a double wall arrangement of the pilot burning zone: this preheated air is turned at the upstream end of the pilot burning zone through swirlers to mix with the original gas and air input (and the liquid fuel input when used) to provide more efficient combustion. One or more fuel injection stages (second stages) are provided for direct input of coal gas into the main burning zone. The countercurrent air coolant passages are connected to swirlers surrounding the input from each second stage to provide additional oxidant.
摘要翻译：描述了用于在燃气轮机中燃烧低BTU煤气的高温燃烧器。燃烧器包括多个单独的燃烧室。每个燃烧室具有主燃烧区和先导燃烧区。用于低BTU煤气的管道连接到先导燃烧区域的上游端：该管道围绕着液体燃料源，并且由供气管道围绕：在液体燃料源和液体燃料源之间设置有旋转装置煤气管道和气体管道和空气管道之间。附加的预热空气由通过主燃烧区的壁的双壁布置形成的通道中的逆流冷却剂空气提供，该主壁与先导燃烧区的双壁布置的通道连通：该预热空气在上游端的先导燃烧区域通过旋流器与原始气体和空气输入（以及使用时的液体燃料输入）混合，以提供更有效的燃烧。提供一个或多个燃料喷射级（第二级），用于将煤气直接输入主燃烧区。逆流空气冷却剂通道连接到围绕来自每个第二级的输入的旋流器以提供附加的氧化剂。

7. 发明授权

US4236378A Sectoral combustor for burning low-BTU fuel gas 失效
标题翻译：用于燃烧低BTU燃气的部门燃烧器
公开(公告)号：US4236378A
公开(公告)日：1980-12-02
申请号：US882073
申请日：1978-03-01
申请人： Robert L. Vogt
发明人： Robert L. Vogt
IPC分类号： F23R3/06 , F23R3/00 , F23R3/36 , F02C7/18
CPC分类号： F23R3/002 , F23R3/36 , F23R2900/00002
摘要： A high-temperature combustor for burning low-BTU coal gas in a gas turbine is disclosed. The combustor includes several separately removable combustion chambers each having an annular sectoral cross section and a double-walled construction permitting separation of stresses due to pressure forces and stresses due to thermal effects. Arrangements are described for air-cooling each combustion chamber using countercurrent convective cooling flow between an outer shell wall and an inner liner wall and using film cooling flow through liner panel grooves and along the inner liner wall surface, and for admitting all coolant flow to the gas path within the inner liner wall. Also described are systems for supplying coal gas, combustion air, and dilution air to the combustion zone, and a liquid fuel nozzle for use during low-load operation. The disclosed combustor is fully air-cooled, requires no transition section to interface with a turbine nozzle, and is operable at firing temperatures of up to 3000.degree. F. or within approximately 300.degree. F. of the adiabatic stoichiometric limit of the coal gas used as fuel.
摘要翻译：公开了一种用于在燃气轮机中燃烧低BTU煤气的高温燃烧器。燃烧器包括几个可单独拆卸的燃烧室，每个燃烧室具有环形横截面和双壁结构，允许由于热效应而由于压力和应力而分离应力。描述了使用在外壳壁和内衬壁之间的逆流对流冷却流动来对每个燃烧室进行空气冷却的布置，并且使用通过内衬板槽和沿着内衬壁表面的膜冷却流，并且将所有冷却剂流体接纳到内衬壁内的气体路径。还描述了用于向燃烧区域供应煤气，燃烧空气和稀释空气的系统，以及用于低负荷运行时使用的液体燃料喷嘴。所公开的燃烧器是完全风冷的，不需要与涡轮喷嘴连接的过渡部分，并且可在高达3000°F的燃烧温度或在所用煤气的绝热化学计量极限的约300°F内操作作为燃料。

8. 发明授权

US5083422A Method of breach cooling 失效
标题翻译：破裂冷却方法
公开(公告)号：US5083422A
公开(公告)日：1992-01-28
申请号：US489627
申请日：1990-03-07
申请人： Robert L. Vogt
发明人： Robert L. Vogt
IPC分类号： F01D5/18 , F23R3/00
CPC分类号： F23R3/002 , F01D5/188 , F05D2260/201 , F23R2900/03044 , Y02T50/67 , Y02T50/676
摘要： The present invention comprises a method and apparatus for improving cooling of a wall in a gas turbine engine. The method and apparatus provide breach cooling of an imperforate wall, such as a combustor liner, for improving the cooling thereof. The breach cooling includes structure for channeling a cooling fluid as a jet toward an outer surface of the imperforate wall, with the jet having sufficient momentum to breach a boundary layer of the cooling fluid which forms over the wall outer surface to allow the jet to contact the wall outer surface for more effective cooling thereof. In an exemplary embodiment of the invention, the breach-cooled wall is an upstream portion of the gas turbine engine combustor, and the inner surface of the combustor liner facing the combustion gases is characterized by not having a film-cooling boundary layer of air to reduce quenching of the combination gases for reducing exhaust emissions.
摘要翻译：本发明包括一种用于改善燃气涡轮发动机中的壁的冷却的方法和装置。该方法和装置提供诸如燃烧器衬套的无孔壁的破裂冷却，以改善其冷却。破裂冷却包括用于将冷却流体作为射流引导到无孔壁的外表面的结构，其中射流具有足够的动量以破坏在壁外表面上形成的冷却流体的边界层，以允许射流接触壁外表面更有效地冷却。在本发明的示例性实施例中，泄漏冷却壁是燃气涡轮发动机燃烧器的上游部分，并且面向燃烧气体的燃烧器衬套的内表面的特征在于不具有膜冷却边界层的空气减少组合气体的淬火以减少废气排放。

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